HORN-R
NORAD 69507
Payload
LEO
2026-132F
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LEO · NORAD 69507
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
521 km
Apogee
548 km
Inclination
97.7°
Period
95.3 min
Mean Motion
15.10520239 rev/day
TLE Epoch
2026-08-03 15:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude535 km
Orbital Velocity27,351 km/h
Velocity7.60 km/s
Orbital Period95 minutes
Orbits / Day15.11
Eccentricity0.0020
Semi-Major Axis6,906 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
2026-06-12
Launch Site
TNSTA
Int'l Designator
2026-132F
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
HORN-R is an active satellite operated by Japan, launched on 2026-06-12 from TNSTA on the VEP-5 launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 521 km and 548 km with an inclination of 97.7°. It travels at approximately 27,351 km/h (7.60 km/s), completing one full orbit every 95 minutes — that’s roughly 15.11 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 years. Orbital Radar tracks HORN-R in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
HORN-R orbits at an average altitude of 535 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of HORN-R’s average altitude, there are currently 2,534 active payloads and 304 tracked debris or rocket body fragments — notable neighbours include STARLINK-1184, STARLINK-1276, STARLINK-1451. This makes it one of the more crowded altitude bands, containing roughly 14.2% of all active satellites. With an inclination of 97.7°, HORN-R passes over latitudes between 97.7°N and 97.7°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. Japan operates approximately 200 active satellites in total, of which 54 share a similar altitude band with HORN-R.
❓ Frequently Asked Questions
HORN-R is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 535 km altitude. Its 97.7° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 95 minutes, travelling at 27,351 km/h.
HORN-R is operated by Japan. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 69507. You can track HORN-R in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
HORN-R was launched on 2026-06-12 from TNSTA. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks HORN-R (NORAD ID 69507) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. Open the live tracker to see its current position, altitude, speed and orbital path updated in real time. You can also browse the satellite directory to find other tracked objects.
HORN-R travels at approximately 27,351 km/h (16,995 mph) — roughly 7.60 km/s. It completes 15.11 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.